A liquid fueled gas generator is described which was designed to simulate the effluent produced by a solid propellant hydrocarbon fuel, typical of those used for ducted rocket propulsion, by burning a very fuel-rich mixture of liquid hydrocarbons with gaseous oxygen. The gas generator was built to function as a tool for the development of components of the ramburner portion of the ducted rocket system and to provide a means for studying the thermochemical processes involved in the production of the fuel-rich effluent and its secondary combustion with air in the ramburner. Successful operation has been documented at total fuel and oxidizer flow rates through the gas generator of 0.20 kg/sec (0.44 lbs/sec) during direct-connect ducted rocket combustion tests.


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    Titel :

    The development of a liquid fueled gas generator for ducted rocket research


    Weitere Titelangaben:

    Entwicklung eines Flüssigkraftstoff-Gasgenerators für Untersuchungen über Raketenantriebe mit Leitungskanälen


    Beteiligte:
    Buckley, P.L. (Autor:in) / Corporan, E. (Autor:in)


    Erscheinungsdatum :

    1991


    Format / Umfang :

    8 Seiten, 5 Bilder, 1 Tabelle, 7 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Performance of ducted rocket

    Kassner, R.R. / Gobetz, F.W. | Engineering Index Backfile | 1960


    Characteristics analysis of solid-liquid ducted rocket

    Lizi, Q. / Shuqiang, L. / Yu, L. | British Library Online Contents | 2010


    Investigation of a Ducted Rocket with a Hybrid Gas Generator

    Gany, A. / Komornik, D. | British Library Conference Proceedings | 2013